Iyi dzidzo yakanyorwa ne Local Solar System Foundation team member uye inogona kuvandudzwa nemunhu ane ruzivo. Une ruzivo rwekutaura nezvenyaya iyi here? Suggest an edit
Mu1903, Konstantin Tsiolkovsky, mudzidzisi wechikoro akataura zvisina kujeka, akanyora pasi equation iyo inoramba ichienzanisa marudzi ese erocket. Izvi zvinotsanangura kuti nei Falcon 9 ichishandiswa ne89% yepropellant, nei payload iri chete muzana rakawanda rehuwandu hwepakutanga, uye nei marockets achisiya zvinhu zvavo panzira.
Yese rocket ndeimwe racing pakati pesimba iwe uchida uye masendimita iwe unofanira kutakura kuti uwane.
Ona
A rocket inofamba nekuvatuka maseva kumashure. Throw zviri nyore, kana throw zvakawanda, uye iwe kuenda nekukurumidza. Kune matambudziko: mafuta asingazivikanwe kuti achiri kusvibiswa, anofanirawo kuendeswa uye kukwira. Izvi zvinoita kuti kuwanikwa kuri logarithmic: kuti udzore simba rakafanana, unofanirwa kusvibisa mafuta, kwete kuisa.
Delta-v (Δv, “change in velocity”) ndiyo mari yendege dzepasi. Ichi chirongwa chinopa mutengo mukm/s:
- Kutanga kubva panyika kusvika kumahombekombe: 9.4 km/s, kusanganisira kushaya simba.
- Low orbit to geostationary orbit: about 3.9 km/s.
- Low orbit kudzokera kuMars: 3.6 km/s.
Roketi yemari ndeyekuti ndezvipi Δv ayo masimba, mafuta uye maseru anogona kupa.
_Zvinyorwa
Δv = I_sp · g₀ · ln(m₀ / m_f)
- I_sp: specific impulse, chiyero chekushanda kwechigadzirwa mumasekondi (kubuda kwemhepo kuparadzwa ne g₀).
- g₀ = 9.80665 m/s², standard gravity.
- m₀: masendimita pakutanga kwekupisa; m_f: masendimita pakupera.
Mufananidzo wekutanga neyakagadzirwa rocket (Isp 348 s): yakazara, inorema makirogiramu 112, kusanganisira 15-makirogiramu payload; pasina propulsant, pamusoro 19 makirogiramu. Δv = 348 × 9.81 × ln(112 / 19) ≈ 6.0 km/s. Chikamu chekutanga chinowedzera zvimwe zvinhu.
A chete chiitiko nechiuru ratio ye10 uye Isp 350 s anopa chete 7.9 km / s, kwete zvakakwana kuti orbit kana kushaya zvinonzi, uye chivakwa kuti ndiro chete 10% yemutengo yakanga iri nyore zvikuru. Izvi ndizvo zvinoita kuti rocket iite makiromita makumi maviri nemana kana kupfuura.
Munyori
Staging inowedzera huwandu hwemafuta. Yechikwata chemotokari,
Δv_total = I₁ g₀ ln(m₁/m_f₁) + I₂ g₀ ln(m₁₂/m_f₂)
apo yekupedzisira-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-yekutanga-ye Kuvandudza kuparadzana pakati pezvirongwa (neimwe Isp, zvakaenzana Δv pachikamu) ndechimwe chematambudziko ekare: payload fraction inokwira nesimba neDv yaunoda, izvo zvinoita kuti kuderedza Δv kuenda kumaorbit nemazana mashoma emamita / s (kutanga kumabvazuva, pedyo neEquator) zviite sezvakakosha.
Equationwo ano explicates pfungwa ye reusable yekutanga zvirongwa: ivo kukwirazve kushandisa mafuta kuti kunge zvakanga payload simba, trading a few percent of payload kuti kwete kubvisa yakanyanya mutengo chikamu cherocket.
Tarisa
Nekushandisa Δv = Isp · g₀ · ln(m₀/m_f), ona kuti ndeipi huwandu hwemafuta anodiwa neimwe-chikamu cherocket ine Isp = 350 s kuti iende 9.4 km/s. Ndeipi chikamu chekubuda kwemhepo chaiyo chinogona kuve nechimiro uye kutakura?
Great. Zvipingamupinyi ndezvekuti kudzidza kunoramba kuripo.
Chidzidzo chekukurukura
3 nhanho mibvunzo. Choose mashoko kuti uone kana iwe uri zvakanaka.
-
Mu equation yerocket, kudhonza kwe mass ratio (m₀/m_f) kunoita sei kune delta-v?
- A Doubles it
- B Inowedzera huwandu hwakafanana (Isp · g₀ · ln 2)
- C Halves it
- D Hapana
Kuratidza mhinduro
B. Inowedzera huwandu hwakafanana (Isp · g₀ · ln 2) Delta-v inokura ne logarithm ye mass ratio: pamwechete kudzokorora kunowedzerawo, pamusoro pe2.4 km/s for Isp 350 s.
-
Chii chinonzi yakakwira-yakaenzana impulse (Isp)?
- A A bigger rocket
- B Yakakwira-yekubuda, saka yakawanda delta-v kubva kune imwe fuel
- C Kuwedzera kumanikidza
- D A heavy engine
Kuratidza mhinduro
B. Yakakwira-yekubuda, saka yakawanda delta-v kubva kune imwe fuel
-
Nei kugadzirira ichibatsira?
- A Vadzidzi vanoenda kunzvimbo dzakaomarara uye vasingagoni kuenda kuno, saka vanoenda kumabasa ezuva nezuva.
- B Inoita kuti rocket ive ne aerodynamic
- C Mapoka anopisa panguva imwe chete
- D Inowedzera mafuta mundege
Kuratidza mhinduro
A. Vadzidzi vanoenda kunzvimbo dzakaomarara uye vasingagoni kuenda kuno, saka vanoenda kumabasa ezuva nezuva.
Kusvika pakupera
- Ona dzidziso
- Akakunda chipingamupinyi
- Akatora chidzidzo
. Kuchengeta kuenderera mberi kwebasa pane iyi kifaa, tinya paKunyora.
Chidzidzo chakapera. Yakanaka!
Kumusoro Hohmann kutumira: kuchinja orbitsMashoko mubhuku rino
Zvinyorwa
- K. Tsiolkovsky, Exploration of Outer Space by Means of Reaction Devices (1903), NASA history summary
- NASA Glenn Research Center, Ideal rocket equation
- SpaceX, Falcon User's Guide (2021)
- H. D. Curtis, Orbital Mechanics for Engineering Students, 4th ed., ch. 13
Iyi dzidzo ine mubhadharo CC BY-SA 4.0.